Presentation 2008-04-25
Mechanism of Radio Wave Attenuation by M-V Rocket Exhaust
Tomohiko SAKAI, Tsutomu OHSHIMA, Teruo KATO, Yukio KAMATA, Zenichi YAMAMOTO,
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Abstract(in English) When a radio wave passes through the rocket exhaust plume, it is attenuated and Phase fluctuation occurs. The amount of attenuation caused by the rocket exhaust plume depends on frequency, motor pressure, atmospheric pressure and attitude of the rocket. We investigated the mechanism of signal attenuation theoretically from the flight data of M-V rocket, and estimated a radio wave model of the plume using electromagnetic field simulation. These results will be applicable to the designs of the rocket telemetry systems in the future.
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Keyword(in English) Rocket Exhaust / Wave Attenuation / Phase fluctuation / M-V Rocket
Paper # SANE2008-4
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Conference Information
Committee SANE
Conference Date 2008/4/18(1days)
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Paper Information
Registration To Space, Aeronautical and Navigational Electronics (SANE)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) Mechanism of Radio Wave Attenuation by M-V Rocket Exhaust
Sub Title (in English)
Keyword(1) Rocket Exhaust
Keyword(2) Wave Attenuation
Keyword(3) Phase fluctuation
Keyword(4) M-V Rocket
1st Author's Name Tomohiko SAKAI
1st Author's Affiliation Institute of Space and Astrnautical Science()
2nd Author's Name Tsutomu OHSHIMA
2nd Author's Affiliation Institute of Space and Astrnautical Science
3rd Author's Name Teruo KATO
3rd Author's Affiliation Institute of Space and Astrnautical Science
4th Author's Name Yukio KAMATA
4th Author's Affiliation Institute of Space and Astrnautical Science
5th Author's Name Zenichi YAMAMOTO
5th Author's Affiliation Institute of Space and Astrnautical Science
Date 2008-04-25
Paper # SANE2008-4
Volume (vol) vol.108
Number (no) 18
Page pp.pp.-
#Pages 6
Date of Issue